RECOVERY AND RESCUE SYSTEM FOR AIRCRAFT

摘要

The recovery and rescue system includes a sail (5) with rigging (10) fitt ed around a spreader conduit (4), with an intake and outlet nozzle, wherein a starting system (6) is provided, including mechanical (12-13) and electrom echanical (17-18) opening mechanisms, in the first case operated by a manual lever (16) and in the second case operated by a button (19). Air driven thr ough the intake of the spreading conduit (4) activates the starting system ( 6) in order to spread the sail (5) and by parachute means retain or brake th e aircraft wherein the said system assembly is fitted. Said system can be ho used inside the aircraft in a container provided for the purpose.